Abstract
Magnetorques and the biased momentum wheel are usual control actuators for microsatellite. The speed of the biased momentum wheel may incline to saturate under a disturbing torque or some demand. Aimed at reducing the probability of making the biased momentum wheel speed to saturate, a designed method of distributive control is proposed, which combines the speed control of the biased momentum wheel and the attitude control in the three-axis stabilization control stage. Through the design of the rational gains, the wheel speed control can be adjusted to be a low dynamic control, which lags far behind the attitude control. The method can optimize the biased momentum wheel speed and reduce the probability of the biased momentum wheel speed saturation. The simulation demonstrates the discussions and can keep the biased momentum wheel in a good state for control.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Wang, P., Zhang, W., Zhang, H., Jie, Wu.: Attitude control of low-orbit microsatellite. J. Natl. Univ. Defense Technol. 33(3), 18–22 (2011)
Jia, F., Wei, Xu., Li, H., Hou, L.: The study of control algorithm for spacecraft attitude control based on the combination of reaction wheels and magnetorque. Aerosp. Control 28(3), 16–19 (2010)
Costic, B.T., Queiroz, M.S., Dawson, D.M., et al.: Energymanagement and Attitude Strategies using Flywheels. Conference Decision and Control, Florida (2001)
Ma, X.: Studyon the Attitude Control System of Satellite with Reaction Wheels and Magnetotors. Harbin Institute of Technology (2013)
Hirota, K., Chen, K.W., Dong, F.Y.: Computational intelligence approachto real-world cooperative vehicle dispatching problem. In: 2nd International IEEE Conference on Intelligent Systems, Varna (2004)
Chen, M., Zhang, S., Zhang, Y.: Combined attitude control method of small satellite using reaction wheels and magnetorquers. J. Jilin Univ. 40(4), 1155–1160 (2010)
Wang, X., Zhang, X.: Attitude control method with a non-biased momentum wheel and magnetorquers. Aerosp. Control Appl. 40(6), 48–50 (2014)
Trégouët, J.-F., Arzelier, D., Peaucelle, D., Pittet, C., Zaccarian, L.: Reaction wheels desaturation using magnetorquers and static input allocation. IEEE Trans. Control Syst. Technol. 23(2), 525–539 (2015)
Hu, S.: Automatic Control Theory, 6th edn., p. 387. Science Press (2013)
Feng, C.: International geomagnetic reference field model calculated by matlab. Inner Monglia Petrochem. Ind. 12, 43–46 (2014)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2022 The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Xiao, W., Li, X., Zhang, N., Zhang, P., Gong, Y., Ma, R. (2022). A Distributive Control Method for Microsatellite Using the Biased Momentum Wheel and Magnetorquers. In: Yan, L., Duan, H., Yu, X. (eds) Advances in Guidance, Navigation and Control . Lecture Notes in Electrical Engineering, vol 644. Springer, Singapore. https://doi.org/10.1007/978-981-15-8155-7_195
Download citation
DOI: https://doi.org/10.1007/978-981-15-8155-7_195
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-15-8154-0
Online ISBN: 978-981-15-8155-7
eBook Packages: Intelligent Technologies and RoboticsIntelligent Technologies and Robotics (R0)